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Airbus A320 > Airbus A320/General > Flashcards

Airbus A320/General Flashcards

1
Q

Max Tailwind A320

A

Takeoff 15 knots

Landing 10 knots

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2
Q

Max Tailwind A319

A

Takeoff 10 knots

Landing 10 knots

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3
Q

Max Cross Wind For Takeoff/Landing

A

38 knots (Including Gusts)

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4
Q

Max TR Load

A

200 Amps

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5
Q

Portable Bottle O2 Minimum Pressure

A

1600 PSI

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6
Q

Max EGT for Engine Start

A

635 EGT

Red Line

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7
Q

Max EGT for Takeoff/G0-Around

A

635 EGT
Red Line
5 min with both engines
10 min with a single engine

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8
Q

Max Continuous EGT

A

610
Yellow Line
Unlimited

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9
Q

Oil Quantity

A

Max Before Start 17 Quarts

Minimum At Idle RPM 12 Quarts

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10
Q

Oil Temps

A 
Max Continuous          155 c
Max for 15 min.            165 c
Min Prior to Start         -40 c
Min Prior to exc Idle    -10 c
Min Prior to Takeoff      50 c
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11
Q

Max RPM

A

N1 100%

N2 100%

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12
Q

Starter Duty Cycle

A

2 min ON / 15 sec OFF
2 min ON / 15 sec OFF
1 min ON / 30 min OFF
5 min ON/ 30 min OFF (continuous cranking)
Start attempt thing is from start valve opening until closing
If open for more than 2 min the ENG MASTER switch must be selected OFF for 30 min.

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13
Q

Max Starter Re-engagement RPM

A

10% N2

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14
Q

APU Altitudes

A

For APU start using battery power only 25,000 ft.
For APU start using normal electrics 39,000 ft.

Two pack operation 15,000 ft.
One Pack operation 20,000 ft.

For Engine start 20,000 ft.

APU Start capability is improved below 31,000 ft.

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15
Q

MAX Flap/Slat Extended Altitude

A

20,000

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16
Q

Speed Brakes Restrictions

A

IMC: Do not use from 1500’ AGL or the FAF whichever occurs latter.

VMC: Do not use below 1000’ AGL

In Flight With Slats Retracted: Do not use below 200 kts.

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17
Q

Fuel Capacity

A

Outer Wing Tanks 3100 lbs
Inner Wing Tanks 25,000 lbs
Center Tank 14,900 lbs

Total 43,000 lbs

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18
Q

Inner Tank Max Imbalance

A

Full 3300 lbs

5,000 5000 lbs

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19
Q

Outer Tank Max Imbalance

A

1520 lbs.

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20
Q

No Option Fuel

A

800 lbs.

Amount required to execute a go-around to 1,000’ AGL. Fly a VFR pattern, intercept a 3 degree glide slope 2.5 miles from the runway.

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21
Q

Fuel Burn (Hours/Min.)

A

Taxi 2 Engine 1500/25
Taxi 1 Engine 900/15

APU:
Supplying neither electrical or pneumatic 160/2.7
Supplying electrical power only 200/3.3
Supplying pneumatic power only 260/4.3
Supplying pneumatic and electric 290/4.8

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22
Q

Fuel Temperature

A

MAX 54 C

MIN -36 C

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23
Q

Max Hydraulic Operating Pressure

A

3200 psi

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24
Q

Icing Condition Exist

A

In flight or on the ground when outside air temperature is 10C or below. In flight use TAT. Visible moisture in any form is present.

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25
Q

Wing Anti-Ice is not permitted when

A

While on the ground

With the use of APU bleed air

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26
Q

Maximum Brake Temp for Takeoff

A

300 C

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27
Q

Max Landing Gear Extended Altitude

A

25,000 ft.

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28
Q

Minimum Tire Pressure for the A320

A

Nose 171 psi

Main 200 psi

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29
Q

Minimum Tire Pressure for the A319

A

Nose 175 psi

Main 180 psi

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30
Q

Max Winds for Auto Land

A

Headwind 30 knots
Crosswind 15 knots
Tailwind 10 knots

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31
Q

Max Pitch Attitude for Auto Pilot Engagement

A

18 degrees ANU

32
Q

Auto Pilot Engagement After Takeoff/Go-around

A

100’ AGL

33
Q

Auto Pilot Engagement Enroute

A

500’ AGL

34
Q

Auto Pilot Engagement Non-precision Approaches

A

250’ AGL

35
Q

Auto Pilot Engagement Non Auto-Land ILS with CAT 1 FMA

A

160’ AGL

36
Q

Auto Pilot Engagement Non Auto-Land ILS with CAT 2 or CAT 3 FMA

A

80’ AGL

37
Q

Auto Pilot Engagement Auto-Land

A

Rollout/Taxi Speed

38
Q

Do not arm ILS APPR mode above

A

8000’

39
Q

In NAV mode, the IRS only provides valid magnetic heading between

A

73 North and 60 South

Flights North of 73N and 60S are prohibited.

40
Q

The use of “Open Descent” is prohibited

A

Inside the FAF on an ILS or non-precision approach or below 1500’ AGL during a visual approach

41
Q

RNAV Approaches are prohibited

A

If the MAP is located prior to the runway threshold.

42
Q

TRK-FPA MODE is not authorized

A

For takeoff and must be deflected during a go-around or missed approach.

43
Q

Pressurization Cabin Differential

A

Negative -1.0 psi

Maximum 8.6 psi

44
Q

Flap/Slat Extended Speeds

A 
Flaps
1                   220
1+F.              205
2.                 190
3.                 175
FULL.           167
45
Q

Max Landing Gear Speed

A

Retraction 220 kts
Extension 250 kts
Extended 280/.67 mach

46
Q

Max Operating Speed

A

350 kts/.82 mach

47
Q

Operation Speed with One or Both FMGCs Operative

A

Climb/Cruse/Descent ECON

Approach Managed Speed

48
Q

Operating Speed with both FMGCs Inoperative

A

Climb/Cruse/Descent .78/290

Approach Selected Vapp

49
Q

Sever Turbulence Speed

A

Above 20,000 .76/275

Below 20,000 250 kts

50
Q

Best Climb Rate

A

280 kts

51
Q

Best Climb Angle

A

Green Dot

52
Q

Max Wind For Passenger Door Operation

A

65 kts

53
Q

Max Tire Speed

A

195 kts ground speed

54
Q

Windshield Wiper Operation Speed

A

230 kts

55
Q

Max Pressure Altitude For Takeoff and Landing

A

9,200

56
Q

Max Operating Altitude

A

39,100

57
Q

Altitude Pax O2 Masks Deploy

A

10,000

58
Q

Max Taxi Weight A320

A

170.6

59
Q

Max Takeoff Weight A320

A

169.7

60
Q

Max Taxi Weight A319

A

167.3

61
Q

Max Takeoff Weight A319

A

166.4

62
Q

Max Landing Weight A320

A

142.2

63
Q

Max Landing Weight A319

A

137.7

64
Q

Max ZFW A320

A

134.4

65
Q

Max ZFW A319

A

128.9

66
Q

APU Starter Duty Cycle

A

1 minute between each start attempt.
60 min cooling time after the third attempt.

*Do not start APU if it has auto shutdown and fueling is in progress

67
Q

Minimum Oil Pressure

A

60 psi

68
Q

Cockpit Window Open Speed

A

200 kts

69
Q

Cockpit Minimum O2 Pressure

A

850 psi

1230 psi on China Airplanes 48xx 49xx

70
Q

ECAM Procedures that must be accomplished using the QRH/Flight Manual

A

AIR ENG 1(2) BLEED ABNORMAL PR
AIR ENG 1(2) BLEED FAULT
F/CTL SPLR FAULT

71
Q

Auto land is not authorized at:

A

Seattle

Anchorage

Fairbanks

St. John’s

Vancouver

For the following A/C: 319 N801-N837
320 N401-N472

72
Q

Autopilot engagement Non-ILS Approach

A

250 AGL

73
Q

Autopilot engagement Circle-To-Land Approach

A

500 AGL

74
Q

Engine warm up: An engine shut down for over two hours must operate near idle for _________ minutes before takeoff.

A

5 minutes

75
Q

Engine run up: both engines need to operate near idle for a minimum of __________ minutes before takeoff

A

2 minutes

76
Q

Engine cool down

A

3 minutes after landing

2 minutes if no more than idle reverse

At the gate brakes set regardless of time

Airbus A320 (25 decks)

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